Conceptual design for a 5 kWe space nuclear reactor power system

被引：0

作者：

Mei, Huaping ^{[1
]}

Yu, Dali ^{[1
]}

Ma, Shengqin ^{[1
,2
]}

Zhang, Jiansong ^{[1
,2
]}

Sun, Yongju ^{[1
]}

Chen, Chao ^{[1
]}

He, Meisheng ^{[1
]}

Wang, Haixia ^{[1
]}

Li, Yang ^{[1
]}

Wang, Liang ^{[1
]}

Li, Taosheng ^{[1
,2
]}

Yu, Jie ^{[1
,2
]}

机构：

[1] Chinese Acad Sci, Hefei Inst Phys Sci, Inst Nucl Energy Safety Technol, Hefei 230031, Peoples R China

[2] Univ Sci & Technol China, Hefei 230027, Peoples R China

来源：

NUCLEAR ENGINEERING AND TECHNOLOGY | 2024年 / 56卷 / 09期

基金：

中国国家自然科学基金;

关键词：

Space nuclear reactor; Heat pipe reactor; Space exploration; Conceptual design;

D O I：

10.1016/j.net.2024.04.015

中图分类号：

TL [原子能技术]; O571 [原子核物理学];

学科分类号：

0827 ; 082701 ;

摘要：

Enhancing the capabilities of unmanned space exploration, such as satellite monitoring and space science missions, requires efficient and reliable nuclear power systems. A viable solution is found in the 1-10 kWe power level of space nuclear reactor power systems, offering advantages such as a manageable research and development process, and relatively low investment requirements. This paper introduces a conceptual design for a 5 kWe space nuclear reactor power system, outlining its components and characteristics. The study includes a thorough analysis of potential challenges, encompassing heat pipe failure accidents, re-entry scenarios, and weight estimation considerations. The results demonstrate that the proposed space nuclear reactor power system effectively meets the safety requirements. The total mass of the power system is estimated at approximately 1.5 tons, with a specific mass of around 300 kg/kWe. This research contributes valuable insights for the design of space nuclear reactor power systems operating within a similar power range.

引用

页码：3644 / 3653

页数：10

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